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NASA Marshall Space Flight Center Human Factors Engineering Analysis of Various Hatch Sizes

机译:美国宇航局马歇尔空间飞行中心人类因素各种舱口尺寸的工程分析

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The NASA Docking System (NDS) is a 31.4961-inch (800 mm) diameter circular hatch for astronauts to pass through when docked to other pressurized elements in space or for entrance or egress on surface environments. The NDS is utilized on the Orion Spacecraft and has been implemented as the International Docking System Standard (IDSS). The EV74 Human Factors Engineering (HFE) Team at NASA's Marshall Space Flight Center (MSFC) conducted human factors analyses with various hatch shapes and sizes to accommodate for all astronaut anthropometries and daily task comfort. It is believed that the hatch, approximately 32 inches, is too small, and a bigger hatch size would better accommodate most astronauts. To conduct human factors analyses, four participants were gathered based on anthropometry percentiles: 1st female, 5th female, 95th male, and 99th male.
机译:美国宇航局对联系统(NDS)是31.4961英寸(800毫米)直径的圆形舱口,用于宇航员,当停靠在空间中的其他加压元件或表面环境中的入口或出口时通过。 NDS在Orion Spacecraft上使用,并已被实施为国际对接系统标准(IDS)。 NASA的马歇尔航天飞行中心(MSFC)的EV74人类因素工程(HFE)团队进行人为因素分析,各种舱口形状和尺寸,以适应所有宇航员人类人类,以及每日任务舒适。据信,舱口,大约32英寸太小,舱口大小更好地容纳大多数宇航员。为了进行人类因素分析,基于人类测量百分位数(第5雌性,第5雌性,第95名男性和第99名男性)聚集了四个参与者。

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